A seat pan for a passenger seat and a passenger seat. The seat pan is corrugated for partially absorbing a downward loading applied to the seat pan through deformation of a corrugation pattern of the seat pan as a result of a counter force applied by a support structure of the passenger seat.
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1. A passenger seat, comprising:
a rigid top seat pan having a corrugation pattern; and
a bottom seat pan;
wherein the rigid top seat pan is disposed above the bottom seat pan for partially absorbing a downward loading applied to the rigid top seat pan through deformation of the corrugation pattern of the rigid top seat pan as a result of a counter force applied by the bottom seat pan.
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This application is a national phase application under 35 U.S.C. §371 of International Application No. PCT/SG2013/000139, filed on Apr. 5, 2013, the disclosure of which is incorporated herein by reference in its entirety.
The present invention relates broadly to a seat pan for a passenger seat and to a passenger seat.
A standard economy-class-type passenger seat for an aircraft comprises of a seat bottom, a reclining seat back and armrests, all supported by structural frames mounted on a laterally spaced-apart leg assembly.
One of the most common causes of injuries experienced in an aircraft crash is by excessive initial loads caused by deceleration, for which loads the materials of the aircraft's underlying support structures and their ability to dissipate energy are the main factors. For example, in a crash scenario, a 14 g downward load may be experienced.
Typically, the leg assembly design has taken into account the 14 g downward load crash scenario. A leg assembly that is too stiff may be able to prevent the seat from collapsing on itself during a crash, keeping the occupants safe from being crushed. However, that stiffness in turn may cause damage to the vital internal organs and spinal column of the passenger, as little energy is attenuated or absorbed during the incident. Conversely, if the leg assembly is too flexible, it would overly deform and fail in a crash.
Embodiments of the present invention seek to provide at least an alternative to existing approaches for addressing the 14 g downward load in a crash scenario.
In accordance with a first aspect of the present invention, there is provided a seat pan for a passenger seat, the seat pan being corrugated for partially absorbing a downward loading applied to the seat pan through deformation of a corrugation pattern of the seat pan as a result of a counter force applied by a frame structure of the passenger seat.
In accordance with a second aspect of the present invention, there is provided a passenger seat comprising a seat pan according to the first aspect.
Embodiments of the invention will be better understood and readily apparent to one of ordinary skill in the art from the following written description, by way of example only, and in conjunction with the drawings, in which:
Embodiments of the present invention relate to a top seat pan that can partially absorb a downward loading applied to the seat pan through deformation of a corrugation pattern of the seat pan as a result of a counter force applied by a frame structure of the passenger seat. In the described embodiments, a passenger can slide the seat pan forward while tilting the forward end of the seat pan slightly upwards and its rear end downwards, with or without simultaneous movement of the seat back assembly, in order to preferably meet various passengers' comfort needs.
As illustrated in
Alternatively, as illustrated in
In an example embodiment, the degree to which the passenger wishes to shift the seat depends on the amount of force applied. The rate at which the seat moves forward in relation to the rate at which the forward end of the top seat pan moves upward and the rear end of the top seat pan moves downward (and thus the seat cushion correspondingly) can be determined by the design of the seat structure including the top seat pan.
With reference to
With reference to
In this embodiment, the top seat pan 202 can advantageously partially absorb a downward loading applied to the top seat pan 202, through deformation of a corrugation pattern of the top seat pan 202 as a result of a counter force applied by the bottom pan 200, as a support structure of the passenger seat 302.
Additionally, and with reference to
In an example embodiment, the curvature 400 is designed such that the centre of gravity, indicated at numeral 402, of most passengers in the seated position is rearward of the centre of curvature, indicated at numeral 404. Therefore, a downward load 406 can force the top seat pan 202 (
The nature of the corrugation of the top seat pan 500 can vary in different embodiments, for example the number, shape and dimensions of pockets e.g. 502 can be varied, to enhance the rigidity as well as the energy attenuation of the seat pan 500. In the example embodiment, the pockets e.g. 502 advantageously serve several purposes in the design of the seat pan 500:
With reference to
Slide guides e.g. 630 are mounted on the bottom pan 602 and are received in tracks e.g. 632 formed on the top pan 604 extending between pockets e.g. 634, 635 of the corrugation pattern, for guiding movement of the top pan 604 relative to the bottom pan 602 when assembled.
In this embodiment, the top seat pan 604 can advantageously partially absorb a downward loading applied to the top seat pan 604, for example in a 14 g downward load scenario, through deformation of the corrugation pattern of the top seat pan 604 as a result of a counter force applied by the bottom pan 604, as a support structure of the passenger seat in this example embodiment.
In this embodiment, an interface 636 to the back seat structure for pushing the top pan 604 during reclining of the seat back extends across the corrugated cross section design of the top pan 604. The interface 636 advantageously receives the push force in such a way as to avoid bending at the interface 636, since the contact point/area is close to, or substantially at, a stiffness center of the top seat pan 604, to advantageously minimize a moment applied for improved durability and smoothness of movement. For example, in this embodiment the stiffness center would be located in the upper half of the interface 636.
The interface between seatback and top seat pan 604 can be designed in other ways in different embodiments, with the translation of the top seat pan 604 preferably being through contact, for achieving independent movement of the top pan 604. In different embodiments, for example varying contact areas, location, patterns etc. may be used.
The components and their installation as described for example embodiments preferably allow easy replacement during maintenance checks, and the design of the components is such that they can be fabricated with ease, as will be appreciated by a person skilled in the art. This advantageously means that while the components may experience wear and tear after prolonged usage, as with all moving components, they can be readily and cost effectively replaced during maintenance checks if required, and/or according to a replacement schedule.
As shown in
In an example embodiment, returning the top seat pan to the default position in preparation for TTOL (Taxing, Take Off and Landing), can be facilitated by installing a biasing member such as a spring or springs, or spring structure(s) between the top, and bottom seat pans, or between the top seat pan and the seat frame. In the following, one non-limiting example will be described.
The top seat pan in the example embodiment can be moved by:
These mechanisms in an example embodiment advantageously allow independent movement of the top seat pan from the seatback when it is not reclined fully, as well as allowing automatic restoration of the seat pan when no force is acting on the top pan. The flexibility of selecting the seating position can preferably provide comfort to a large population passenger profile.
In addition to retracting the top seat pan back to its default position once e.g. the passenger's applied force is removed, the biasing means such as the spring or springs can advantageously also act as an energy absorption system during instances of rapid deceleration in the forward direction, such as the 16 g forward loading condition, via compression, which can enhance the survivability of the passenger. Furthermore, the energy absorbing springs can help reduce the forward distance travelled by the passenger's head in such an event. This is believed to be because preferably the head moves with the body against the spring or springs first, with the forward inertia being partially absorbed by the spring or springs. This can reduce the amount of travelling distance by the body and head as a whole, before the head may move further relative to the body due to any remaining energy.
With reference to
The bottom pan 802 in this example is fabricated to span the width of a multi-seat configuration, e.g. a triple seat configuration. Each top pan 804 is supported by the bottom pan 802. It is noted that the top pan 804 is corrugated, for example like the top pan 504 described above with reference to
With reference to
Slide guides e.g. 930 are mounted on the bottom pan 902 and are received in tracks e.g. 932 formed on the top pan 904 extending between pockets e.g. 934, 935 of the corrugation pattern, for guiding movement of the top pan 904 relative to the bottom pan 902 when assembled.
In this embodiment, an interface 936 to the back seat structure for pushing the top pan 904 during reclining of the seat back extends across the corrugated cross section design of the top pan 904. The interface 936 advantageously receives the push force in such a way as to avoid bending at the interface 936, since the contact point/area is close to, or substantially at, a stiffness center of the top seat pan 904, to advantageously minimize a moment applied for improved durability and smoothness of movement. For example, in this embodiment the stiffness center would be located in the upper half of the interface 936.
The interface between seatback and top seat pan 904 can be designed in other ways in different embodiments, with the translation of the top seat pan 904 preferably being through contact, for achieving independent movement of the top pan 904. In different embodiments, for example varying contact areas, location, patterns etc. may be used.
In one embodiment, a seat pan for a passenger seat is provided, the seat pan being corrugated for partially absorbing a downward loading applied to the seat pan through deformation of a corrugation pattern of the seat pan as a result of a counter force applied by a support structure of the passenger seat. The seat pan can be corrugated along one or more directions thereof. The seat pan can gave a curvature configured to substantially match a curvature of the support structure. The curvature can be along a depth of the seat pan. The curvature can be between first and second opposing ends with an intermediate portion between the first and second ends, the intermediate portion being at a vertically lower position compared to the first and second ends, relative to the passenger seat.
In one embodiment, the seat pan is moveable relative to the support structure in forward and backward directions with reference to the frame structure. The seat pan can further be configured for receiving a force exerted by a seat back of the passenger seat for movement of the seat pan relative to the support structure. The seat pan can be configured to receive a pushing force exerted by the seat back. The seat pan can be configured to receive the pushing force as a result of reclining of the seat back.
In one embodiment, the seat pan can comprise an interface structure disposed for receiving the force. The interface structure can comprise a substantially flat surface for receiving the force. The interface structure can comprise a surface with a recess formed therein for receiving the force. The interface structure can be disposed at one end of the seat pan and can extend substantially across the corrugation pattern of the seat pan.
In one embodiment, the seat pan comprises one or more rollers for engaging one or more track strips mounted to the support structure.
In one embodiment, the seat pan comprises one or more track strips for engaging one or more rollers mounted to the support structure.
In one embodiment, the seat pan comprises one or more slider elements for being received in corresponding one or more guiding tracks mounted to the support structure.
In one embodiment, the seat pan comprises one or more guiding tracks for receiving one or more corresponding slider elements mounted to the support structure.
In one embodiment, the seat pan further comprises one or more retaining structures for limiting movement of the seat pan. Each restraining structure can comprise a first element on the seat pan for abutting a second element mounted to the support structure. The seat can further comprise biasing means for biasing the seat pan in a default position. The biasing means can comprise one or more springs.
In one embodiment, the support structure comprises a further seat pan of the passenger seat, and the seat pan is configured to be disposed above the further seat pan. The seat pan can be configured for being moveable relative to a frame structure of the passenger seat independent from movement of a seat back of the passenger seat.
It will be appreciated by a person skilled in the art that numerous variations and/or modifications may be made to the present invention as shown in the specific embodiments without departing from the spirit or scope of the invention as broadly described. The present embodiments are, therefore, to be considered in all respects to be illustrative and not restrictive.
For example, the retainer can be designed in other ways that sliding is allowed while sufficient holding strength has been provisioned through the design. Examples include varying locations, mechanical fastening methods. Preferably, the retainer design provides for securing the top seat pan in 16 g as well as 14 g situations.
As another example, the seat pans can be designed with different corrugation patterns, different shapes, different material as well as different processes to achieve desired moving patterns. Also, the biasing means can be provided differently, including using springs selected and installed with different stiffness, and/or at different locations to best suit an overall effect in accordance with the seat design in example embodiments.
Zheng, Guo Ying, Baz, Charles Fakhri, Sawada, Teruo
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Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
Apr 05 2013 | Singapore Technologies Aerospace Ltd | (assignment on the face of the patent) | / | |||
Apr 05 2013 | Tenryu Aero Component Co., Ltd. | (assignment on the face of the patent) | / | |||
Nov 06 2015 | BAZ, CHARLES FAKHRI | TENRYU AERO COMPONENT CO , LTD | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 037168 | /0335 | |
Nov 06 2015 | BAZ, CHARLES FAKHRI | Singapore Technologies Aerospace Ltd | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 037168 | /0335 | |
Nov 09 2015 | ZHENG, GUO YING | TENRYU AERO COMPONENT CO , LTD | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 037168 | /0335 | |
Nov 09 2015 | SAWADA, TERUO | Singapore Technologies Aerospace Ltd | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 037168 | /0335 | |
Nov 09 2015 | ZHENG, GUO YING | Singapore Technologies Aerospace Ltd | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 037168 | /0335 | |
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Jan 06 2018 | Singapore Technologies Aerospace Ltd | TENRYU AERO COMPONENT CO , LTD | CHANGE OF NAME SEE DOCUMENT FOR DETAILS | 047749 | /0667 | |
Jan 06 2018 | Singapore Technologies Aerospace Ltd | ST ENGINEERING AEROSPACE LTD | CHANGE OF NAME SEE DOCUMENT FOR DETAILS | 047749 | /0667 | |
Nov 19 2020 | TENRYU AERO COMPONENT CO , LTD | ST ENGINEERING AEROSPACE LTD | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 054653 | /0378 |
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